Orbital elements of GOSAT 2
| Launched | 28 October 2018 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 43672 |
| Alternative names |
IBUKI 1 |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| 2026 Feb 05 18:58 | 2026 Feb 05 07:02:58 | 97.8677 | 0.00014 | 9.9673 | 91.1201 | 269.0170 | 14.84251 | – |
| 2026 Feb 04 18:57 | 2026 Feb 04 06:46:47 | 97.8674 | 0.00015 | 9.9008 | 94.7445 | 269.0170 | 14.84251 | – |
| 2026 Feb 03 18:56 | 2026 Feb 03 06:30:37 | 97.8680 | 0.00018 | 9.8345 | 106.7387 | 269.0170 | 14.84251 | – |
| 2026 Feb 02 18:56 | 2026 Feb 02 07:51:31 | 97.8677 | 0.00015 | 9.7723 | 92.3773 | 269.0170 | 14.84251 | – |
| 2026 Feb 01 18:56 | 2026 Feb 01 07:35:20 | 97.8677 | 0.00015 | 9.7058 | 93.7802 | 269.0170 | 14.84251 | – |
| 2026 Jan 31 18:56 | 2026 Jan 31 07:19:10 | 97.8674 | 0.00015 | 9.6393 | 94.5589 | 269.0170 | 14.84251 | – |
| 2026 Jan 30 18:57 | 2026 Jan 30 07:02:59 | 97.8675 | 0.00015 | 9.5728 | 88.1786 | 269.0170 | 14.84251 | – |
| 2026 Jan 29 18:56 | 2026 Jan 29 06:46:49 | 97.8675 | 0.00015 | 9.5063 | 89.3130 | 269.0170 | 14.84251 | – |
| 2026 Jan 28 18:56 | 2026 Jan 27 19:11:06 | 97.8670 | 0.00016 | 9.4087 | 90.3524 | 269.0170 | 14.84251 | – |
| 2026 Jan 27 18:56 | 2026 Jan 27 07:51:33 | 97.8670 | 0.00016 | 9.3777 | 90.7768 | 269.0170 | 14.84251 | – |
| 2026 Jan 26 18:57 | 2026 Jan 26 07:35:22 | 97.8670 | 0.00016 | 9.3112 | 91.7229 | 269.0170 | 14.84251 | – |